Engineering:Intelsat VA F-11
| Mission type | Communication |
|---|---|
| Operator | Intelsat |
| COSPAR ID | 1985-055A [1] |
| SATCAT no. | 15873 |
| Mission duration | 7 years (planned) |
| Spacecraft properties | |
| Bus | Intelsat VA |
| Manufacturer | Ford Aerospace |
| Launch mass | 1981 kg |
| Dry mass | 1098 kg [2] |
| Dimensions | 1.66 x 2.1 x 1.77 metres |
| Power | 1800 watts |
| Start of mission | |
| Launch date | 30 June 1985, 00:44:00 UTC [3] |
| Rocket | Atlas G (AC-64) |
| Launch site | Cape Canaveral Air Force Station , LC-36B |
| Contractor | General Dynamics |
| End of mission | |
| Disposal | Graveyard orbit |
| Deactivated | August 2003 |
| Orbital parameters | |
| Reference system | Geocentric orbit[1] |
| Regime | Geostationary orbit |
| Longitude | 27.5° West (1985-1991) [4] 63.0 East (1991-1992) 177.0° East (1992-1995) 180.0° East (1995-1998) 29.5° West (1998-2003) |
| Epoch | 30 June 1985 |
| Transponders | |
| Band | 26 C-band 6 Ku-band |
Intelsat V | |
Intelsat VA F-11, then named Intelsat 511, was a communications satellite operated by Intelsat. Launched in 1985, it was the eleventh of fifteen Intelsat V satellites to be launched. The Intelsat VA series was constructed by Ford Aerospace, based on the Intelsat VA satellite bus. Intelsat VA F-11 was part of an advanced series of satellites designed to provide greater telecommunications capacity for Intelsat's global network.
Satellite
The satellite was box-shaped, measuring 1.66 by 2.1 by 1.77 metres; solar arrays spanned 15.9 metres tip to tip. The arrays, supplemented by nickel-hydrogen batteries during eclipse, provided 1800 watts of power at mission onset, approximately 1280 watts at the end of its seven-year design life. The payload housed 26 C-band and 6 Ku-band transponders. It could accommodate 15,000 two-way voice circuits and two TV channels simultaneously. It also provided maritime communications for ships at sea.[5]
Launch
The satellite was successfully launched into space on 30 June 1985, at 00:44:00 UTC, by means of an Atlas G-Centaur-D1AR vehicle from the Cape Canaveral Air Force Station , Florida, United States . It had a launch mass of 1981 kg.[4] The satellite was deactivated in August 2003.
References
- ↑ 1.0 1.1 "Display: Intelsat 5A F-11 1985-055A". NASA. 14 May 2020. https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=1985-055A.
This article incorporates text from this source, which is in the public domain.
- ↑ "Intelsat-5A". Gunter's Space Page. http://space.skyrocket.de/doc_sdat/intelsat-5a.htm.
- ↑ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. http://planet4589.org/space/log/launchlog.txt.
- ↑ 4.0 4.1 "Intelsat 511". TSE. http://www.tbs-satellite.com/tse/online/sat_intelsat_511.html.
- ↑ "Display: Intelsat 5A F-15 1989-086A". NASA. 14 May 2020. https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=1989-006A. This article incorporates text from this source, which is in the public domain.
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